Methods are described for launching multiple space vehicles. A first space vehicle and a second space vehicle can be detachably attached to a launch vehicle. The first space vehicle is for an orbit of a first desired altitude in a first desired orbital plane. The second vehicle is for an orbit of a second desired altitude in a second desired orbital plane. The launch vehicle with the first and second space vehicles may be launched into a first orbit in or near the first desired orbital plane. The second space vehicle may be released in the first orbit. When the orbital plane of the second space vehicle coincides with the second desired orbital plane, the second space vehicle may be transferred to a transfer orbit. The second space vehicle may be transferred to the orbit of the second desired altitude in the second desired orbital plane.